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<title> NACA 63(2)-415 (Velux Measurements) </title></head>

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<H1>NACA 63<font size="-1">(2)</font>-415 AIRFOIL</H1>
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Reynolds number = 1.6 x 10^6 <br><br>

Measured at Velux wind tunnel (see <A
HREF="./../HTML/biblio.htm#FuglsangASM">Fuglsang, Antoniou, S&oslash;rensen
and Madsen</A>) <br><br>

More details on computations and experimental facilities can be found in
the <A HREF="./../HTML/report.htm"><font color="#006699">Wind Turbine
Airfoil Catalogue</font></A>.


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<H1>DATA AVAILABLE:</H1><p><p>

- <A HREF="./prof.dat"> Airfoil shape </A><p>

<font size=+3> Experiments:<br> </font>
- <A HREF="./cldm.exp"> Lift, Drag and Moment Coefficients </A><p>

- <A HREF="./cp_05.95.exp"> Pressure Distribution - Angle of Attack = 05.95 deg. </A><br>
- <A HREF="./cp_08.43.exp"> Pressure Distribution - Angle of Attack = 08.43 deg. </A><br>
- <A HREF="./cp_10.42.exp"> Pressure Distribution - Angle of Attack = 10.42 deg. </A><br>
- <A HREF="./cp_12.33.exp"> Pressure Distribution - Angle of Attack = 12.33 deg. </A><br>
- <A HREF="./cp_15.19.exp"> Pressure Distribution - Angle of Attack = 15.19 deg. </A><br>
- <A HREF="./cp_17.59.exp"> Pressure Distribution - Angle of Attack = 17.59 deg. </A><p>

<font size=+3> XFOIL Computations:<br> </font>
- <A HREF="./cldm.xf"> Lift, Drag and Moment Coefficients </A><p>
- <A HREF="./cfp_05.95.xf"> Skin Friction and Pressure Distributions - Angle of Attack = 05.95 deg. </A><br>
- <A HREF="./cfp_08.43.xf"> Skin Friction and Pressure Distributions - Angle of Attack = 08.43 deg. </A><br>
- <A HREF="./cfp_10.42.xf"> Skin Friction and Pressure Distributions - Angle of Attack = 10.42 deg. </A><br>
- <A HREF="./cfp_12.33.xf"> Skin Friction and Pressure Distributions - Angle of Attack = 12.33 deg. </A><br>
- <A HREF="./cfp_15.19.xf"> Skin Friction and Pressure Distributions - Angle of Attack = 15.19 deg. </A><br>
- <A HREF="./cfp_17.59.xf"> Skin Friction and Pressure Distributions - Angle of Attack = 17.59 deg. </A><p>

<font size=+3> EllipSys2D Computations: </font><p>
<font size=+2><em>* Fully turbulent:</em><br> </font>
- <A HREF="./FULLYTURB/cldm.ellipsys"> Lift, Drag and Moment Coefficients </A><p>
- <A HREF="./FULLYTURB/cp_05.95.ellipsys"> Pressure Distribution - Angle of Attack = 05.95 deg. </A><br>
- <A HREF="./FULLYTURB/cp_08.43.ellipsys"> Pressure Distribution - Angle of Attack = 08.43 deg. </A><br>
- <A HREF="./FULLYTURB/cp_10.42.ellipsys"> Pressure Distribution - Angle of Attack = 10.42 deg. </A><br>
- <A HREF="./FULLYTURB/cp_12.33.ellipsys"> Pressure Distribution - Angle of Attack = 12.33 deg. </A><br>
- <A HREF="./FULLYTURB/cp_15.19.ellipsys"> Pressure Distribution - Angle of Attack = 15.19 deg. </A><br>
- <A HREF="./FULLYTURB/cp_17.59.ellipsys"> Pressure Distribution - Angle of Attack = 17.59 deg. </A><p>

- <A HREF="./FULLYTURB/cf_05.95.ellipsys"> Skin Friction Distribution - Angle of Attack = 05.95 deg. </A> <br>
- <A HREF="./FULLYTURB/cf_08.43.ellipsys"> Skin Friction Distribution - Angle of Attack = 08.43 deg. </A> <br>
- <A HREF="./FULLYTURB/cf_10.42.ellipsys"> Skin Friction Distribution - Angle of Attack = 10.42 deg. </A> <br>
- <A HREF="./FULLYTURB/cf_12.33.ellipsys"> Skin Friction Distribution - Angle of Attack = 12.33 deg. </A> <br>
- <A HREF="./FULLYTURB/cf_15.19.ellipsys"> Skin Friction Distribution - Angle of Attack = 15.19 deg. </A> <br>
- <A HREF="./FULLYTURB/cf_17.59.ellipsys"> Skin Friction Distribution - Angle of Attack = 17.59 deg. </A> <p>

<font size=+2><em>* With transition model:</em><br> </font>
- <A HREF="./TRANSITION/cldm.ellipsys"> Lift, Drag and Moment Coefficients </A><p>
- <A HREF="./TRANSITION/cp_05.95.ellipsys"> Pressure Distribution - Angle of Attack = 05.95 deg. </A><br>
- <A HREF="./TRANSITION/cp_08.43.ellipsys"> Pressure Distribution - Angle of Attack = 08.43 deg. </A><br>
- <A HREF="./TRANSITION/cp_10.42.ellipsys"> Pressure Distribution - Angle of Attack = 10.42 deg. </A><br>
- <A HREF="./TRANSITION/cp_12.33.ellipsys"> Pressure Distribution - Angle of Attack = 12.33 deg. </A><br>
- <A HREF="./TRANSITION/cp_15.19.ellipsys"> Pressure Distribution - Angle of Attack = 15.19 deg. </A><br>
- <A HREF="./TRANSITION/cp_17.59.ellipsys"> Pressure Distribution - Angle of Attack = 17.59 deg. </A><p>

- <A HREF="./TRANSITION/cf_05.95.ellipsys"> Skin Friction Distribution - Angle of Attack = 05.95 deg. </A> <br>
- <A HREF="./TRANSITION/cf_08.43.ellipsys"> Skin Friction Distribution - Angle of Attack = 08.43 deg. </A> <br>
- <A HREF="./TRANSITION/cf_10.42.ellipsys"> Skin Friction Distribution - Angle of Attack = 10.42 deg. </A> <br>
- <A HREF="./TRANSITION/cf_12.33.ellipsys"> Skin Friction Distribution - Angle of Attack = 12.33 deg. </A> <br>
- <A HREF="./TRANSITION/cf_15.19.ellipsys"> Skin Friction Distribution - Angle of Attack = 15.19 deg. </A> <br>
- <A HREF="./TRANSITION/cf_17.59.ellipsys"> Skin Friction Distribution - Angle of Attack = 17.59 deg. </A>


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<H1>FIGURES AVAILABLE: (PostScript files)</H1><p><p>

- <A HREF="./../NACA-WS/NACA-63-415/PS/profile.ps"> Airfoil shape </A><p>

- <A HREF="./PS/cl.ps"> Lift Coefficient </A><br>
- <A HREF="./PS/cd.ps"> Drag Coefficient </A><br>
- <A HREF="./PS/cm.ps"> Moment Coefficient </A><p>

- <A HREF="./PS/cp_a05.95.ps"> Pressure Distribution - Angle of Attack = 05.95 deg. </A><br>
- <A HREF="./PS/cp_a08.43.ps"> Pressure Distribution - Angle of Attack = 08.43 deg. </A><br>
- <A HREF="./PS/cp_a10.42.ps"> Pressure Distribution - Angle of Attack = 10.42 deg. </A><br>
- <A HREF="./PS/cp_a12.33.ps"> Pressure Distribution - Angle of Attack = 12.33 deg. </A><br>
- <A HREF="./PS/cp_a15.19.ps"> Pressure Distribution - Angle of Attack = 15.19 deg. </A><br>
- <A HREF="./PS/cp_a17.59.ps"> Pressure Distribution - Angle of Attack = 17.59 deg. </A><p>

- <A HREF="./PS/cf_a05.95.ps"> Skin Friction Distribution - Angle of Attack = 05.95 deg. </A><br>
- <A HREF="./PS/cf_a08.43.ps"> Skin Friction Distribution - Angle of Attack = 08.43 deg. </A><br>
- <A HREF="./PS/cf_a10.42.ps"> Skin Friction Distribution - Angle of Attack = 10.42 deg. </A><br>
- <A HREF="./PS/cf_a12.33.ps"> Skin Friction Distribution - Angle of Attack = 12.33 deg. </A><br>
- <A HREF="./PS/cf_a15.19.ps"> Skin Friction Distribution - Angle of Attack = 15.19 deg. </A><br>
- <A HREF="./PS/cf_a17.59.ps"> Skin Friction Distribution - Angle of Attack = 17.59 deg. </A><p>



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